摘要
本文对有无控制增稳系统飞机的横航向模态特性进行了比较计算.通过计算对系统进行了数学分析,从而得到了一组较佳的系统参数,提高了系统改善飞机横航向模态特性的能力.
In this Paper, the contents of a CAS (Control Augmentation System) and without CAS of aircraft lateral-directional mode response were computed and compared. Through computing, the system was analysed of methematical, a group better parameter of system were acquired, the system improve a capability of aircraft for lateral-directional mode response was increase.
出处
《飞行力学》
CSCD
北大核心
1989年第3期60-65,共6页
Flight Dynamics
